Power conversion system for nuclear power generators and related methods

ABSTRACT

A power conversion system for converting thermal energy from a heat source to electricity is provided. The system includes a chamber including an inner shroud having an inlet and an outlet and defining an internal passageway between the inlet and the outlet through which a working fluid passes. The chamber also includes an outer shroud substantially surrounding the inner shroud. The chamber includes a source heat exchanger disposed in the internal passageway, the source heat exchanger being configured to receive a heat transmitting element associated with the heat source external to the chamber, and to transfer heat energy from the heat transmitting element to the working fluid. The system also includes a compressor disposed adjacent the inlet of the inner shroud and configured to transfer energy from the compressor to the working fluid, and an expander disposed adjacent the outlet of the inner shroud.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation of U.S. Non-Provisional Pat.Application No. 17/988,771, filed on Nov. 17, 2022, which is acontinuation of U.S. Non-Provisional Pat. Application No. 16/641,229,filed on Feb. 21, 2020, which is a U.S. National Stage Application ofPCT International Application No. PCT/US18/49282, filed on Aug. 31,2018, which claims priority to U.S. Provisional Pat. Application No.62/552,532, filed on Aug. 31, 2017. Contents of the above-mentionedapplications are incorporated herein by reference in their entirety.

TECHNICAL FIELD

The present disclosure relates generally to nuclear power generators. Inparticular, various embodiments of the present disclosure relate topower conversion systems and methods for use in nuclear powergenerators.

DESCRIPTION OF RELATED ART

A nuclear power generator contains a nuclear core for producing thermalenergy during normal operation. After shutdown, the nuclear core stillproduces decay heat, and the amount of decay heat after shutdown isgenerally proportional to the power generation history and power densityof the nuclear core. To avoid overheating of the nuclear core aftershutdown, decay heat energy must be transferred from the nuclear core byredundant heat transfer mechanisms, which are generally supplied bydecay heat removal systems external to the nuclear core. These heattransfer systems may require complex piping networks to connect thepressure vessel containing the nuclear core to heat exchangers generallylocated far away from the pressure vessel. Further, the coolantcirculating between the nuclear core and the heat exchangers may beeither actively circulated by electrically driven pumps and/or blowersor passively circulated via gravity-driven natural circulationmechanisms.

Independent of their sizes, modern nuclear reactors rely on redundantdecay heat removal systems that are generally combinations of passiveand active systems. These systems are formed by components that aregenerally external to the pressure vessel containing the nuclear coreand, therefore, result in a complex system of redundant piping, valves,and heat exchangers for passive systems with the addition ofpumps/blowers and motive power managed and monitored by control systemsand cabling.

Many advanced reactor designs include melt-resistant nuclear coresequipped with various passive heat transfer mechanisms. While providinghighly reliable heat source, however, these nuclear cores may be sealedwithin their pressurized vessels and, therefore, conventional heatremoval systems with complex networks of balance-of-plant components maynot be suitable for use with these advanced reactor designs.

SUMMARY

Therefore, various exemplary embodiments of the present disclosure mayprovide an improved power conversion system that can effectively andefficiently remove heat from a nuclear core while eliminating asubstantial amount of balance-of-plant typically present in aconventional nuclear power generator.

To attain the advantages and in accordance with the purpose of theinvention, as embodied and broadly described herein, one aspect of theinvention may provide a power conversion system for converting thermalenergy from a heat source to electricity. The power conversion systemmay include a substantially sealed chamber having an inner shroud havingan inlet and an outlet and defining an internal passageway between theinlet and the outlet through which a working fluid passes. The sealedchamber may also include an outer shroud substantially surrounding theinner shroud, such that the working fluid exiting the outlet of theinner shroud returns to the inlet of the inner shroud in a closed-loopvia a return passageway formed between an external surface of the innershroud and an internal surface of the outer shroud. The power conversionsystem may further include a source heat exchanger disposed in theinternal passageway of the inner shroud, the source heat exchanger beingconfigured to at least partially receive a heat transmitting elementassociated with the heat source external to the substantially sealedchamber, the source heat exchanger being further configured to transferheat energy from the heat transmitting element to the working fluidpassing through the source heat exchanger.

In another exemplary aspect, the power conversion system may alsoinclude a compressor disposed adjacent the inlet of the inner shroud andconfigured to transfer energy from the compressor to the working fluid,and an expander disposed adjacent the outlet of the inner shroud andconfigured to extract heat energy from the working fluid. In someexemplary aspects, the compressor and the expander may be disposedinside the outer shroud.

According to another exemplary aspect, a power conversion system forconverting thermal energy from a heat source to electricity may comprisea shroud having an inlet and an outlet and defining an internalpassageway between the inlet and the outlet through which a workingfluid passes. The power conversion system may also include a source heatexchanger disposed in the internal passageway of the shroud, the sourceheat exchanger being thermally coupled to a heat transmitting element ofthe heat source and being configured to transfer heat energy from theheat transmitting element to the working fluid passing through thesource heat exchanger.

The power conversion system may also include a compressor disposedadjacent the inlet of the shroud and configured to transfer energy fromthe compressor to the working fluid, and an expander disposed adjacentthe outlet of the shroud and configured to extract heat energy from theworking fluid. In one exemplary aspect, the compressor and the expandermay be disposed inside the shroud.

According to another exemplary aspect, the power conversion system mayinclude an inlet conduit extending from a source of the working fluid toan inlet of the compressor, and a discharge conduit extending from anoutlet of the expander to the source of the working fluid.

Additional objects and advantages of the invention will be set forth inpart in the description that follows, and in part will be obvious fromthe description, or may be learned by practice of the invention.

It is to be understood that both the foregoing summary description andthe following detailed description are exemplary and explanatory onlyand are not restrictive of the invention.

BRIEF DESCRIPTION OF THE DRAWINGS

The accompanying drawings, which are incorporated in and constitute apart of this specification, illustrate several embodiments of theinvention and together with the description, serve to explain theprinciples of the disclosed invention.

FIG. 1 is a functional schematic of a power conversion system disposedinside a transport container, according to an exemplary embodiment ofthe present disclosure.

FIG. 2 is a functional schematic of the power conversion system of FIG.1 , illustrating its main components in more detail.

FIG. 3 is a functional schematic of a sealed chamber having a sourceheat exchanger configured to receive heating elements of a nuclearreactor core, according to one exemplary embodiment.

FIG. 4 is an exploded view of area A shown in FIG. 3 , illustrating anexemplary configuration of a heat transmitting element of a nuclearreactor core and a heat receiving portion of a source heat exchanger.

FIG. 5 is a functional schematic of a power conversion system, accordingto another exemplary embodiment, consistent with the present disclosure.

FIG. 6 is a functional schematic of a power conversion system, accordingto still another exemplary embodiment, consistent with the presentdisclosure.

FIG. 7 is a cross-sectional view of a power conversion system, accordingto still another exemplary embodiment, consistent with the presentdisclosure.

FIG. 8 is a cross-sectional view of a power conversion system, accordingto still another exemplary embodiment, consistent with the presentdisclosure.

DETAILED DESCRIPTION OF EXEMPLARY EMBODIMENTS

Reference will now be made in detail to the exemplary embodiments of theinvention, examples of which are illustrated in the accompanyingdrawings. Wherever possible, the same reference numbers will be usedthroughout the drawings to refer to the same or like parts.

FIGS. 1 and 2 illustrate a power conversion system 1, according to oneexemplary embodiment of the present disclosure. As shown in FIG. 1 ,power conversion system 1, consistent with the present disclosure, maybe sufficiently compact to fit inside a transport container 1 a (e.g.,intermodal container), thereby making it easily transportable by anyconventional transportation means, such as, for example, trucks, freightrails, and ships. Transport container 1 a may include a plurality ofpads 28 located at its bottom surface to provide a stable supportplatform from the ground. Pads 28 may be adjustable in height and mayinclude a vibration dampening mechanism. Pads 28 also thermally separatethe bottom portions of transport container 1 a from the ground, orplatform to be placed under the transport container 1 a, to thermallyinsulate the container 1 a bottom portions from heating said ground orplatform.

Power conversion system 1 may include a closed-loop primary system forconverting thermal energy from a nuclear reactor core to electricity.The thermal energy from a nuclear reactor core is depicted as a heatsource 3 in FIG. 1 , which may represent a heat transmitting portion ofa nuclear reactor. The heat transmitting portion of the nuclear reactormay be a portion of the nuclear reactor core designed to transmit heatdirectly therefrom (e.g., nuclear fuel rods) or a part of anyintermediary structure for transferring heat from the nuclear reactorcore (e.g., heat pipes extending from a reactor core to remove heat fromthe reactor core). As will be described in more detail, power conversionsystem 1 of the present disclosure may be configured to interface withthe heat transmitting portion of the nuclear reactor to remove heattherefrom and convert it into electricity. It should be understood,however, that power conversion system 1 of the present disclosure may beconfigured for other various types of thermal energy. For example, heatsource 3 may alternatively or additionally comprise any other type ofheat generating source, such as, for example, combustion heat fromfossil fuel or geothermal heat.

In the exemplary embodiment shown in FIG. 1 , heat source 3 (e.g., anuclear reactor core) may be disposed underground, such that powerconversion system 1 of the present disclosure may be transported to thesite and positioned directly above heat source 3. It should beunderstood that heat source 3 may be positioned above ground, and powerconversion system 1 may be readily re-configured to accommodatedifferent locations and configurations of heat source 3.

Referring to FIG. 1 , power conversion system 1 may comprise asubstantially sealed chamber 50 having an inner shroud 5 and an outershroud 6 substantially surrounding inner shroud 5. Sealed chamber 50 mayenable pressurization of the closed-loop for working fluid 4 tocirculate, without mixing with fluids potentially operating with heatsource 3. Sealed chamber 50 may also include a source heat exchanger 2inside inner shroud 5. Source heat exchanger 2 may be configured to atleast partially receive a heat transmitting element 3 a of heat source3, such that heat from heat transmitting element 3 a may be transferredto working fluid 4 inside source heat exchanger 2. The portion of sourceheat exchanger 2 that receives heat transmitting element 3 a may includeone or more recesses or pockets (depending on the configuration of heattransmitting element 3 a) extending inwardly from a first flange 22 ofsealed chamber 50, which is outside of the pressure boundary of sealedchamber 50 in which working fluid 4 circulates. Therefore, although heattransmitting element 3 a is thermally coupled to working fluid 4 insidesealed chamber 50, it may not be in direct contact with working fluid 4.

In the exemplary embodiment shown in FIGS. 3 and 4 , heat transmittingelement 3 a may comprise a plurality of heat pipes 3 a extending fromheat source 3 (e.g., a nuclear reactor core), and source heat exchanger2 may comprise a plurality of recesses 2 a extending from first flange22 and configured to receive the plurality of heat pipes 3 a. Sourceheat exchanger 2 may define a plurality of heating channels 2 b throughwhich working fluid 4 may pass. As working fluid 4 passes throughheating channels 2 b, heat from heat pipes 3 a may be transferred toworking fluid 4.

Heat source 3 may include a second flange 23 configured to thermally andhydraulically couple heat source 3 to first flange 22, while allowingthermal expansion and contraction therebetween. First flange 22 andsecond flange 23 can also be configured to dampen vibrations generatedby the operations of power conversion system 1. In some exemplaryembodiments, at least one of first flange 22 and second flange 23 maycomprise a flexible member that may also enhance sealing the gap betweenfirst flange 22 and second flange 23.

Power conversion system 1 may include an electronic controller 24,configured to control and regulate thermodynamic and electricalparameters of the Brayton cycle and the Rankine cycle of transportablepower conversion system 1. The operational characteristics of controller24 will be described in connection with the descriptions of variousrelated components of power conversion system 1.

Each recess 2 a of source heat exchanger 2 may be slightly larger thanheat pipe 3 to form a gap between the outer surface of heat pipe 3 andthe inner surface of recess 2 a. The gap or clearance may allow heatpipe 3 and recess 2 a to expand and contract without inducing mechanicalstress. Recess 2 a may contain a suitable heat transfer medium 2 c inthe gap, which may enhance heat transfer between heat pipe 3 and recess2 a. Heat transfer medium 2 c may also ensure that heat pipe 3 andrecess 2 a remain in thermal contact during expansion and contraction.

As shown in FIGS. 1 and 5 , inner shroud 5 may include an inlet 5 a andan outlet 5 b and define an internal passageway between inlet 5 a andoutlet 5 b through which working fluid 4 can pass. Source heat exchanger2 may be disposed inside the internal passageway of inner shroud 5between inlet 5 a and outlet 5 b to exchange heat energy with heattransmitting element 3 a of heat source 3. As will be described in moredetail herein, when working fluid 4 flows through source heat exchanger2, heat energy from heat source 3 is transferred to working fluid 4without working fluid 4 physically mixing with any working fluid of heatsource 3. Working fluid 4 may comprise any suitable working fluid withadequate thermal-physical properties to operate under a Brayton- orRankine-cycle thermodynamic configuration.

Power conversion system 1 may further include a compressor 7 disposedadjacent inlet 5 a of inner shroud 5 and an expander 10 disposedadjacent outlet 5 b of inner shroud 5. Compressor 7 may compriseturbomachinery components, such as, for example, multi-stage statornozzles and rotary turbines or positive displacement components,configured to transfer energy from compressor 7 to working fluid 4 bycompressing and/or pumping working fluid 4. Expander 10 may compriseturbomachinery components, such as, for example, multi-stage statornozzles and rotary turbines or positive displacement components,configured to extract heat energy from working fluid 4.

Outer shroud 6 may substantially surround inner shroud 5, compressor 7,and expander 10. Outer shroud 6 may define a return passageway betweenthe outer surface of inner shroud 5 and the inner surface of outershroud 6. The return passageway may be configured to guide working fluid4 exiting expander 10 to recirculate back to compressor 7. Outer shroud6 may also be configured to structurally support the turbomachinerycomponents of compressor 7 and expander 10.

Outer shroud 6 may also provide mechanical coupling and support forelectric motor 9 and electric generator 12, while defining a sealedflange (not shown) enabling rotation of the rotary components ofcompressor 7 and expander 10. In some exemplary embodiments, outershroud 6 may be configured to provide mechanically support for, anddefine fluid dynamic pathways of, stators 7 a, 10 a (FIG. 5 ) of rotaryturbomachinery components. Similarly, inner shroud 5 may be configuredto provide mechanical support for, and define fluid dynamic pathways of,stators 7 a and 10 a of the rotary turbomachinery components for workingfluid 4 to be compresses by compressor 7.

Before entering inlet 5 a of inner shroud 5, working fluid 4 iscompressed and/or pumped by compressor 7. Working fluid 4 then entersinlet 5 a of inner shroud 5, passes through heating channels 2 b ofsource heat exchanger 2 to extract heat energy from one or more heattransmitting elements 3 a, and exits outlet 5 b of inner shroud 5.Working fluid 4 exiting outlet 5 a of inner shroud 5 enters expander 10and expands through the turbomachinery components of expander 10.Working fluid 4 discharged from expander 10 passes through the returnpassageway defined by inner shroud 5 and outer shroud 6 and recirculatesback to compressor 7.

As shown in FIGS. 1 and 2 , compressor 7 may comprise a motor shaft 8configured to mechanically couple the rotary components of compressor 7to an electric motor 9. Compressor 7 is driven by electric motor 9, andelectric motor 9 is driven by a portion of the electricity produced byan electric generator 12 conditioned by a conditioner 17. Expander 10may comprise a generator shaft 12 configured to mechanically couple therotary components of expander 10 to electric generator 12. Expander 10is driven by working fluid 4 flowing from source heat exchanger 2 andexiting inner shroud 5. Electric generator 12 may comprise powerelectronic components, such as, for example, IGBT-based inverters, andmay produce electricity rectified and conditioned by conditioner 17.Conditioner 17 may also regulate the electricity produced by electricgenerator 12 to supply the conditioned electricity to a power bus 18 andto electric motor 9. The rotary components of compressor 7 and motorshaft 8 and the rotary components of expander 10 and second rotarycomponent 11 may form distinct turbo-machinery rotary componentsoptimized to pump/compress or expand independently of one another.

In the disclosed exemplary embodiment, electric motor 9 and electricgenerator 12 may be cooled by a motor cooling circuit 9 a (FIG. 2 ) anda generator cooling circuit 12 a, respectively. Motor cooling circuit 9a and generator cooling circuit 12 a may use a working fluid 14different from working fluid 4 of the closed-loop primary system.Working fluid 14 may comprise a thermal-oil, an organic fluid, or anyfluid with adequate thermal-physical properties to operate within thetemperature and pressure ranges suitable for the Brayton- andRankine-cycle components of power conversion system 1.

As best shown in FIG. 2 , motor cooling circuit 9 a may comprise arecirculation pump 9 c configured to recirculate working fluid 14, amotor heat exchanger 9 b configured to receive thermal energy generatedby electric motor 9, and a radiator 9 f configured to transfer thermalenergy from electric motor 9 to the ultimate heat sink. In thisexemplary embodiment, motor cooling circuit 9 a may include a set ofthree-way valves 9 d to transfer working fluid 14 to a secondaryconversion system having components operating under a Rankine cycle(hereinafter referred to as Rankine engine 20) by hydraulic tubing 9 e.

Similarly, generator cooling circuit 12 a may comprise a recirculationpump 12 c configured to recirculate working fluid 14, a generator heatexchanger 12 b configured to receive thermal energy generated byelectric generator 12, and a radiator 12 f configured to transferthermal energy from electric generator 12 to the ultimate heat sink. Inthis exemplary embodiment, generator cooling circuit 12 a may include aset of three-way valves 12 d configured to regulate the mass flow rateof working fluid 14 flowing to and from Rankine engine 20 via hydraulictubing 12 e.

Three-way valves 9 d of motor cooling circuit 9 a and three-way valves12 d of generator cooling circuit 12 a may be controlled by controller24. The working fluid circulating through motor cooling circuit 9 a andgenerator cooling circuit 12 a may be different than working fluid 14.Any fluid with suitable thermal-physical properties for Rankine engine20 can be used.

Rankine engine 20 may comprise a recuperator 16 configured to transferthermal energy from working fluid 4 to working fluid 14. Ranking engine20 may also comprise a pump 33 configured to pressurize working fluid14, a condenser 34 configured to transfer thermal energy from workingfluid 14 to the ultimate heat sink (e.g., environmental air), anexpander 20 a configured to expand working fluid 14 and convert thermalenergy into mechanical energy, and a generator 20 b coupled to expander20 a and configured to convert mechanical energy from expander 20 a intoelectrical energy 18 a. Electrical energy 18 a may be conditioned bycontroller 24. Expander 20 a may comprise multi-stage turbomachinerycomponents or positive displacement components.

In one exemplary embodiment, Rankine engine 20 may be thermally coupledto working fluid 4 by positioning at least a portion of recuperator 16in a return passageway 35 (FIG. 2 ) between the outer surface of innershroud 5 and the inner surface of outer shroud 6. Alternatively oradditionally, recuperator 16 may be thermally coupled to outer shroud 6.In another exemplary embodiment, recuperator 16 may include a pluralityof heat transfer fins 41 for thermally coupling working fluid 4 inreturn passageway 35 to recuperator 16. Overall, the components ofRankine engine 20 may be thermally coupled to working fluid 4 andthermally and hydraulically coupled to working fluid 14 and dischargethermal energy to the ultimate heat sink. The ultimate heat sink may beenvironmental air, or water if power conversion system 1 is submergedunder water.

In some exemplary embodiments, a portion of recuperator 16 may bethermally coupled to a plurality of extended fins 41 a that may extendto source heat exchanger 2, such that recuperator 16 is directlythermally coupled to heat transmitting element 3 a. Rankine engine 20with this exemplary configuration may enable decay heat removal fromheat source 3 by exchanging decay heat energy with the ultimate heatsink.

Rankine engine 20 may be thermally and hydraulically coupled to motorcooling circuit 9 a to recover thermal energy generated by electricmotor 9 and may regulate, via three-way valves 9 d, operationalparameters of working fluid 14, such as, for example, pressure,temperature, and mass-flow-rate. Similarly, Rankine engine 20 may alsobe thermally and hydraulically coupled to generator cooling circuit 12 ato recover thermal energy generated by generator 12 and may regulateoperational parameters of working fluid 14 via three-way valves 12 d.

For configurations where the ultimate heat sink is environmental air 15,one or more passive or active cooling devices 25, such as, for example,cooling fans, may be used to circulate heated air 15 a and cool down theheat exchangers of intercooler 26 and recuperator 16. Cooling devices 25may be regulated by controller 24. In some exemplary embodiments,cooling devices 25 may be positioned to direct environment air 15 toflow upwardly from the bottom to the top to take advantage of buoyancyforces as it changes density proportionally to its temperature.Environment air 15 exchanges thermal energy with condenser 34 and heattransfer surfaces 1 c of transportable container 1 a.

According to another exemplary embodiment, environment air 15 may flowsideways with respect to transport container 1. In still anotherexemplary embodiment, environment air 15 may flow into and out from thetop portion of transport container 1 a.

In some exemplary embodiments, compressor 7 may include an intercooler26 configured to exchange energy between working fluid 4 and workingfluid 14. As shown in FIG. 2 , Rankine engine 20 may be thermallycoupled to intercooler 26 to recover waste thermal energy generated bycompressor 7 by regulating the flow of working fluid 14. In oneexemplary embodiment, controller 24 may be configured to control one ormore valves 27 to regulate the flow of working fluid 14. Intercooler 26may use working fluid 14 a different from working fluid 14 of Rankineengine 20.

FIG. 5 schematically illustrates a power conversion system 100,according to another exemplary embodiment of the present disclosure.This exemplary embodiment may differ from the exemplary embodimentsshown in FIGS. 1 and 2 in that, among other things, power conversionsystem 100 may employ an open-loop system for converting thermal energyfrom heat source 3 to electricity. For example, as will be described inmore detail herein, power conversion system 100 may utilize anintermediary thermodynamic system 30 a for transferring heat energy fromheat source 3 to source heat exchanger 2.

As shown in FIG. 5 , intermediary thermodynamic system 30 a may comprisean intermediary vessel 29 to which a plurality of heat transmittingelements 3 a may extend from heat source 3. Intermediary vessel 29 maybe filled with a suitable medium 2 c for effectively removing heat fromheat transmitting elements 3 a. Although not illustrated in detail,intermediary vessel 29 may include a suitable structure for interfacingwith heat source 3. For example, intermediary vessel 29 may include aninterface structure similar to first flange 22 and second flange 23 ofpower conversion system 1 shown in FIGS. 1 and 2 . In an alternativeembodiment, intermediary vessel 29 and heat source 3 may form a unitarypressure boundary in which medium 2 c of intermediary vessel 29 mixeswith a coolant inside heat source 3.

To transfer the heat from intermediary vessel 29, intermediarythermodynamic system 30 a may include an intermediary heat exchanger 2 ddisposed inside intermediary vessel 29, or thermally coupled to vessel29. Intermediary thermodynamic system 30 a may also include an auxiliarypump 38 configured to circulate a working fluid 30, an actuator 40configured to control the flow of working fluid 30, and a pressurizer 39configured to maintain pressure of working fluid 30 and/or toaccommodate temperature-induced volume changes of working fluid 30.Accordingly, working fluid 30 is configured to transfer thermal energyfrom intermediary vessel 29 to source heat exchanger 2. Working fluid 30may comprise a liquid metal or any other suitable fluid with properthermal-physical properties. In one exemplary embodiment, working fluid30 may be the same as working fluid 14. In still another exemplaryembodiment, working fluid 30 may be the same as working fluid 4.

Power conversion system 100 may comprise a first flange 22 configured tothermally and hydraulically connect to heat source 3 via intermediarythermodynamic system 30 a. First flange 22 may comprises at least oneinlet port 22 a and at least one outlet port 22 b for hydraulicallyconnecting intermediary heat exchanger 2 d to source heat exchanger 2.

As shown in FIG. 5 , source heat exchanger 2 may be disposed insideinner shroud 5 that is, in this configuration, exposed to the fluidsrepresenting the ultimate heat sink. In other words, inner shroud 5 maydefine an open internal passageway between inlet 5 a and outlet 5 bthrough which a fluid representing the ultimate heat sink (e.g.,environment air or water) may flow. In this exemplary embodiment, powerconversion system 100 may comprise an inlet conduit 36 extending fromthe ultimate heat sink (e.g., outside of transport container 1 a) to acompressor inlet 36 a. Similarly, power conversion system 100 maycomprise a discharge conduit 37 extending from an expander outlet 37 ato the ultimate heat sink.

Power conversion system 100 may include a recuperator 16 configured totransfer thermal energy from heated fluid 15 a discharged from expander10 to working fluid 14 circulating in Rankine engine 20. Recuperator 16may be disposed within, or otherwise thermally coupled to, dischargeconduit 37 and, as the heat source of Rankine engine 20, may beconfigured to extract heat from heated fluid 15 a. Variousturbomachinery components in power conversion system 100 of FIG. 5 maybe similar to those shown and/or described with reference to FIGS. 1 and2 and, therefore, any detailed description will be omitted herein.

As described above, the open-loop thermodynamic cycle executed bycompressor 7 and expander 10 utilizes fluid 15 from the ultimate heatsink. As fluid 15 enters compressor 7 at inlet 36 a, it is compressedand then flown into source heat exchanger 2 to remove thermal energyfrom working fluid 30 of intermediary thermodynamic system 30 a. Fluid15 then expands through expander 20 to convert the thermal energy inheated fluid 15 a into electrical energy via electrical generator 12.Heated fluid 15 a then flows through expander outlet 37 a and transfersthermal energy to recuperator 16 prior to exiting discharge conduit 37.

FIG. 6 schematically illustrates a power conversion system 200,according to another exemplary embodiment of the present disclosure.Similar to power conversion system 100 shown in FIG. 5 , powerconversion system 200 of this exemplary embodiment is an open-loopsystem utilizing the fluid of the ultimate heat sink to convert thermalenergy from heat source 3 to electricity. Power conversion system 200may differ from power conversion system 100 of FIG. 5 in that, amongother things, source heat exchanger 2 can be directly thermally coupledto heat transmitting elements 3 a of heat source 3.

FIG. 7 illustrates a cross-section view of a power conversion system 1,according to still another exemplary embodiment consistent with thepresent disclosure. In this exemplary embodiment, intercooler 26 may bepositioned in the internal passageway of working fluid 4 (forclosed-loop configurations) or fluid 15 of ultimate heat sink (foropen-loop configurations) inside inner shroud 5, and recuperator 16 maysubstantially surround outer shroud 6 and intercooler 26. Accordingly,the working fluid used to convert thermal energy from heat source 3 canbe either working fluid 4 circulating in a closed-loop configuration orfluid 15 taken from the ultimate heat sink (e.g., the environmentsurrounding transport container 1 a) in an open-loop configuration.

In an open-loop configuration, environment air may be suctioned andcompressed by compressor 7. The energy added to the air by compressor 7may be removed by intercooler 26, which may transfer this removed energyto Rankine engine 20 for executing waste heat recovery functions. Thecompressed air flows through source heat exchanger 2 to increase itsenergy content and expands through expander 10. As the air is dischargedat the outlet of expander 10, it may exchange energy with recuperator16, which transfers the recovered energy to Rankine engine 20 forfurther conversion into electricity. Rankine engine 20 may then rejectthermal energy to the ultimate heat sink via one or more cooling device25.

FIG. 8 illustrates a cross-sectional view of a power conversion system100, according to still another exemplary embodiment. Power conversionsystem 100 of FIG. 8 may be an open-loop system, where fluid 15 (e.g.,environment air) may be drawn into compressor 7 through inlet portspositioned substantially in the upper portion (e.g., on the top surface)of transport container 1 a.

While the present invention is described herein with reference toillustrative embodiments for particular applications, it should beunderstood that the invention is not limited thereto. The precedingdescription of the disclosed embodiments is provided to enable anyperson skilled in the art to make or use the claims. Variousmodifications to these embodiments will be readily apparent to thoseskilled in the art, and the generic principles defined herein may beapplied to other embodiments and implementations.

What is claimed is: 1-18. (canceled)
 19. A power conversion system forconverting thermal energy from a heat source to electricity, comprising:an inner shroud including an inlet and an outlet; an inlet conduit andan outlet conduit respectively hydraulically coupled to the inlet andthe outlet of the inner shroud for an environmental working fluid toflow through the inlet conduit, a space enclosed by the inner shroud,and the outlet conduit; a compressor disposed adjacent the inlet of theinner shroud, and configured to suction the environmental working fluidinto the inlet conduit from an external environment, and compress theenvironmental working fluid into the space enclosed by the inner shroudthrough the inlet; a source heat exchanger configured to transferthermal energy to the compressed environmental working fluid to heat upthe compressed environmental working fluid; a flange configured to seala portion of the inner shroud, the flange including an inlet port and anoutlet port; an intermediary thermodynamic system configured to transferthermal energy from a heat source to the source heat exchanger throughthe inlet port and outlet port; wherein the intermediary thermodynamicsystem includes: a pump configured to circulate a working fluid withinthe intermediary thermodynamic system; an intermediary heat exchangerconfigured to transfer thermal energy from the heat source to theworking fluid circulating within the intermediary thermodynamic system;a heat transfer medium thermally coupled to the intermediary heatexchanger and the heat source; and an intermediary pressure vesselconfigured to store and transfer thermal energy from the heat source tothe heat transfer medium; an expander disposed adjacent the outlet ofthe inner shroud and configured to convert thermal energy of the heatedenvironmental working fluid exiting the outlet into rotative energy; andan electric generator mechanically coupled with the expander andconfigured to convert the rotative energy into electricity.
 20. Thepower conversion system of claim 19, wherein the inlet conduit ispositioned radially with respect to the compressor.
 21. The powerconversion system of claim 19, wherein the inlet conduit is positionedaxially with respect to the compressor.
 22. The power conversion systemof claim 19, wherein the compressor includes multistage rotarycomponents and stator components with the stator components mechanicallycoupled to the inner shroud.
 23. The power conversion system of claim22, wherein the compressor includes an intercooler heat exchangerconfigured to cool down the environmental working fluid by thermalexchange.
 24. The power conversion system of claim 23, wherein theintercooler heat exchanger is configured to transfer thermal energy fromthe environmental working fluid flowing through the compressor to cooldown the environmental working fluid before the environmental workingfluid is compressed into the space enclosed by the inner shroud.
 25. Thepower conversion system of claim 19, wherein the source heat exchangeris configured to transfer thermal energy from the heat source to theenvironmental working fluid.
 26. The power conversion system of claim19, wherein the expander includes multistage rotary components andstator components, with the stator components mechanically coupled tothe inner shroud, to expand the heated environmental working fluid. 27.The power conversion system of claim 19, wherein the multistage rotarycomponents of the expander are mechanically coupled to the electricgenerator.
 28. The power conversion system of claim 19, wherein the heatsource includes a nuclear reactor.
 29. The power conversion system ofclaim 19, wherein the pump is configured to circulate the working fluidthrough the source heat exchanger and the intermediary heat exchanger.30. The power conversion system of claim 19, further comprising a pumpconfigured to circulate a working fluid to execute a Rankine engine. 31.The power conversion system of claim 19, further comprising arecuperator heat exchanger configured to transfer thermal energy fromthe heated environmental working fluid exiting from the outlet to aworking fluid circulating in a Rankine engine, to convert the thermalenergy into conditioned electricity.
 32. The power conversion system ofclaim 19, further comprising an electric conditioner configured toregulate the electricity generated by the electric generator.
 33. Asystem, comprising: a power conversion system for converting thermalenergy from a heat source to electricity, the power conversion systemcomprising: an inner shroud including an inlet and an outlet; an inletconduit and an outlet conduit respectively hydraulically coupled to theinlet and the outlet of the inner shroud for an environmental workingfluid to flow through the inlet conduit, a space enclosed by the innershroud, and the outlet conduit; a compressor disposed adjacent the inletof the inner shroud, and configured to suction the environmental workingfluid into the inlet conduit from an external environment, and compressthe environmental working fluid into the space enclosed by the innershroud through the inlet; a source heat exchanger configured to transferthermal energy to the compressed environmental working fluid to heat upthe compressed environmental working fluid; a flange configured to seala portion of the inner shroud, the flange including an inlet port and anoutlet port; an intermediary thermodynamic system configured to transferthermal energy from a heat source to the source heat exchanger throughthe inlet port and outlet port; wherein the intermediary thermodynamicsystem includes: a pump configured to circulate a working fluid withinthe intermediary thermodynamic system; an intermediary heat exchangerconfigured to transfer thermal energy from the heat source to theworking fluid circulating within the intermediary thermodynamic system;a heat transfer medium thermally coupled to the intermediary heatexchanger and the heat source; and an intermediary pressure vesselconfigured to store and transfer thermal energy from the heat source tothe heat transfer medium; an expander disposed adjacent the outlet ofthe inner shroud and configured to convert thermal energy of the heatedenvironmental working fluid exiting the outlet into rotative energy; andan electric generator mechanically coupled with the expander andconfigured to convert the rotative energy into electricity; and atransport container containing the power conversion system.
 34. Thesystem of claim 33, further comprising a condenser heat exchanger, andwherein at least one surface of the transport container is thermallycoupled to the condenser heat exchanger.
 35. The system of claim 33,further comprising a fan disposed in the transport container to force aflow of an environmental fluid to and from an interior of the transportcontainer.
 36. A system, comprising: a chamber; a heat exchangerdisposed inside the chamber; a heat source disposed outside of thechamber and thermally coupled with the heat exchanger; and a rotatorydevice configured to move a working fluid in the chamber to flow throughthe heat exchanger to exchange thermal energy with the heat exchanger.